Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
Short SC7 (Skyvan) Series Aeroplanes
AD/SC7/24 Main Landing Gear Shock Absorber Attachment Pin 10/95
Applicability: All Skyvan MK 3, 3A, 3M and Skyliner series aircraft fitted with main landing gear type numbers EH1831-D, EH1832-D, EH1837-B, EH1838-B, EH1885-1 and EH1886-1.
Requirement: Replace the main landing gear shock absorber attachment pin P/N EH183113 with a new pin of the same P/N or with a new design pin, P/N 200621639.
Note: CAA(UK) AD 004-04-81 refers.
Compliance: If pin P/N EH183113 has exceeded 5280 landings, replace before 14 November 1995 or before 300 landings after 14 September 1995, whichever is the sooner.
Continue to replace pin P/N EH183113 at 5280 landing intervals, replace pin P/N 200621639 at 23 000 landing intervals.
Background: A life limitation has been established on main landing gear shock absorber attachment pin. Installation of a new part number pin provides a substantial increase in fatigue life.
We try to embed the page this law was scraped from. If the site blocks framing, you still get the link and a local excerpt.
Last checked with source on —
Checking whether the official page can be embedded…
Plain-English simplify of this law: a short summary, key points, and both sides of the argument. Generated on first view via Replicate, then cached. Vote on what helps your study.
No study brief is cached for this law yet. Sign up to generate a plain-English brief.
Sign up to generate